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GALLEY BRAKES SYS 2 FUEL AFT XFR
F. STBY PMP 1 F. STBY PMP 2 FUEL PUMP 3
FUEL PUMP 4 F T.tK PUMP R WNDW HEAT
ZONE CTLR 2 FCDC 2 RUD TRIM 2
RUD TRV LIM 2 YAW DAMPER 2 TURB DAMPER
FCMC 2 BMC 1+4 ENG 1+2+3+4 LOOP B
Other INOP SYS
CARGO SQUIB B SFCC 2 SDCU 2
CDLS F/O WIPER F/O RAIN REP.
ENG 1+2+3+4 SQUIB B PACK 2 REGUL RMP 2
PART COCKPIT LTS
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1) (if CH B in control on ENG 1 or 4)
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 121/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT (Cont'd)
(2) (if CH B in control on ENG 2)
(3) (if CH B in control on ENG 3)
ELEC DC BUS 2 FAULT
Applicable to: ,
AIR DATA SWTG (IF ADR 3 AVAIL)...................................................................................F/O ON 3
FM SOURCE.................................................................................................................... BOTH ON 1
SEC 2.................................................................................................................................KEEP ON
L2Note: SEC 2 is normally supplied by DC BUS 2. In case of a DC BUS 2 failure, the DC ESS
BUS supplies SEC 2. However, in this case, the SEC 2 FAULT light, on the overhead
panel, comes on. Do not attempt a reset: Selecting OFF would result in a loss of the SEC
2 backup power supply.
L1 IF CG AFT 32 %, AND WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
L2Note: If the trim tank pump is inoperative, apply the action if the CG is aft of 32 %, and when
the SPD is greater than 270 kt, and not in climb.
L1
SECONDARY FAILURES
*F/CTL
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 122/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT (Cont'd)
L12
STATUS
IF CG AFT 32 %, WHEN SPD > 270 KT AND NOT IN
CLIMB:
T TANK MODE................................................................ FWD
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
BOTH PFD ON SAME FMGEC
PACK 2 AT FIXED TEMP
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
PRIM 2 BMC 2 ZONE CTLR 2
FCDC 2 CAB PR 2 GALLEY
FCMC 2 ENG 1+2 LOOP B F T.TK PUMP
R WSHLD HEAT R WNDW HEAT HALF SPLRS
REV 2 F/O TAT FM 2
TR 2 CAT 3 DUAL Y ELEC PUMP
AP 2 (FMGC 2) VHF 2 LGCIU 2
FUEL AFT XFR L+R F/O STAT HEAT R FUEL PUMP 1
L FUEL PUMP 1 BRAKES SYS 2
Other INOP SYS
PACK 2 REGUL SDCU 2 BRAKE TEMP IND (1 to 4)
CARGO SQUIB B F/O WIPER F/O RAIN REP.
ENG 1+2 SQUIB B AUTOBRAKE SFCC 2
RMP 2 PART COCKPIT LTS CDLS
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 123/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT
Applicable to:
AIR DATA SWTG (IF ADR 3 AVAILABLE)..........................................................................F/O ON 3
FM SOURCE.................................................................................................................... BOTH ON 1
PRIM 2............................................................................................................................... KEEP ON
L2Note: PRIM 2 is normally supplied by DC BUS 2. In case of DC BUS 2 failure, DC BUS 1
supplies the PRIM 2.
However, in this case, the PRIM 2 FAULT light, on the overhead panel, comes on. Do not
attempt a reset: The OFF selection would result in a loss of the PRIM 2 backup power
supply.
L1
SECONDARY FAILURES
*F/CTL
AIR DATA SWTG (IF ADR 3 AVAIL)...................................................................................F/O ON 3
FM SOURCE.................................................................................................................... BOTH ON 1
SEC 2.................................................................................................................................KEEP ON
L2Note: SEC 2 is normally supplied by DC BUS 2. In case of a DC BUS 2 failure, the DC ESS
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(10)
